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METHOD FOR THE DETERMINATION OF AERODYNAMIC COEFFICIENTS WHEN SIMULATING AIRCRAFT AT AVIATION TRAINING DEVICE

机译:在航空训练设备上模拟飞机时确定空气动力学系数的方法

摘要

A method for the determination of aerodynamic coefficients when simulating aircraft at aviation training device consists in that by means of hardware and software tools of aviation training device performed is the correction of aerodynamic coefficients of aircraft flight dynamics computer model using simplex-planning method. Variable values of aerodynamic coefficients of forces and momentums of aircraft spatial motion recorded by airborne device for flight information registration are rated, initial simplex is selected and difference between parameters of real attitude position and identical parameters simulated by aviation training device hardware and software is plotted using aircraft motion dynamic equation. Then optimum assessed values of recurrent simplex are determined with minimization of a discrepancy between required and calculated values thereof to given value, matrix of corrections for approximate model of standard aircraft at aviation training device, and computer model of aircraft flight dynamics at aviation training device is corrected.
机译:一种在航空训练装置上模拟飞机时确定空气动力系数的方法,其特征在于,利用单纯的规划方法,通过执行航空训练装置的硬件和软件工具校正飞机飞行动力学计算机模型的空气动力系数。评估机载设备记录的用于飞行信息登记的航空器空间运动的空气动力和动量空气动力学系数的可变值,选择初始单纯形,并绘制真实姿态位置的参数与由航空训练设备硬件和软件模拟的相同参数之间的差异飞机运动动力学方程。然后,通过最小化其所需值和计算值与给定值之间的差异,确定航空训练设备处标准飞机的近似模型的校正矩阵以及航空训练设备处的飞机飞行动力学的计算机模型,确定递归单纯形的最佳评估值。更正的。

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